Monitoring of fluid flow

ABSTRACT

A method and apparatus for generating a rate of flow signal which is proportional to the flow rate in a fluid distribution system and which is based on a signal which is proportional to the speed of the fluid circulating device and which makes use of the characteristic curves of a fluid circulating system and fluid delivery device is disclosed. In an air-conditioning system having a variable speed supply fan and a variable speed return fan, a method and apparatus for controlling the capacity of the return fan to closely match that of the supply fan is provided. The method comprises the steps of; monitoring the supply fan speed and discharge pressure and generating a first signal which is a measure of the supply fan capacity at the monitored speed, matching the return fan capacity with the supply fan capacity to achieve any required ratio of return fan output to supply fan output and generating a second signal which is a measure of the desired return fan speed required to provide the return fan output and driving the return fan at the measured speed indicated by the second signal.

This application is a continuation of application Ser. No. 571,747, filed 01/18/84, now abandoned which is a continuation-in-part of application Ser. No. 491,878 filed May 5, 1983 now abandoned.

This invention relates to a method and apparatus for determining the fluid flow in a fluid distribution system.

The method and apparatus of the present invention is particularly suitable for use in determining the rate of flow of air in a variable air flow fan system which has a variable speed fan, such as an air conditioning system.

The method and apparatus of the present invention is also suitable for use in determining the rate of flow of liquid in a variable liquid flow pump system which has a variable speed pump.

PRIOR ART

The need for a simple, inexpensive and direct method of indicating flow in an air circulating system or a liquid circulating system is well known.

In air circulating systems such as air conditioning systems the rate of flow is usually measured by installing a duct traverse consisting of a series of flow tubes with a pitot tube in each flow tube. The signal from each flow tube is averaged, and summed. Since this signal varies as the square of the flow, the square root must be taken. This output may then be used to indicate air flow.

The problem with this approach is that each stage of signal processing introduces errors. Also, the most economical computation systems are pneumatic. Manufacturers of this type of system claim an accuracy of about + or -7% with a newly calibrated system. The reason for this inaccuracy is the problem of obtaining accurate signals from a duct traverse. The accuracy will deteriorate further if the computation circuits drift with age or if the pitot tubes become clogged in use. Substituting electronic computation circuits for pneumatic ones will result in less drift, but the maximum error of about + or -7% may not be appreciably decreased.

SUMMARY OF INVENTION

Using the characteristic curves of a fluid circulating system and fluid delivery device I have developed a simple and accurate method of generating a rate of flow signal which is proportional to the flow rate in a fluid distribution system and which is based on a signal which is proportional to the speed of the fluid circulating device.

In addition I have designed a simple and accurate rate of flow signal generating means for generating a rate of flow signal which is proportional to the flow rate in a fluid distribution system and which is based on a signal which is proportional to the speed of operation of the fluid circulating device.

My method and control system is much simpler than that previously available and has a greater accuracy with essentially no deterioration in accuracy with time.

According to one aspect of the present invention there is provided in a fluid circulating system which includes a conduit for conveying the fluid from a fluid delivery device which provides a variable volume fluid discharge by varying the speed of operation of the fluid delivery device, and wherein it is necessary to generate a rate of flow signal which is proportional to the volume of fluid delivered by the fluid delivery device in use, the improved method of generating said rate of flow signal comprising the steps of;

(i) generating a first signal which is proportional to the speed of the fluid delivery device,

(ii) inputting the first signal to a curve fitter which is programmed with the combined fluid delivery device/system speed/flow charcteristic curves of the system and to output an output signal which is proportional to fluid flow delivered by the fluid delivery device.

According to a further aspect of the present invention there is provided in a fluid circulating system which includes a conduit for conveying the fluid from a fluid delivery device which provides a variable volume fluid discharge by varying the speed of operation of the fluid delivery device, and means for generating a first signal which is proportional to the speed of the fluid delivery device, and wherein it is necessary to generate a rate of flow signal which is proportional to the volume of fluid delivered by the fluid delivery device in use, the improvement of means for generating said rate of flow signal comprising;

(i) a curve fitter having an input and an output, said input communicating with said means for generating said first signal, said curve fitter being programmed with the combined fluid delivery device/system speed/flow characteristic curves of the system and being adapted to receive said first signal and to generate a second signal which is proportional to fluid flow delivered by the fluid delivery device, said second signal being discharged at said output.

According to yet another aspect of the present invention there is provided in a an air circulating system which includes a duct for conveying air from a variable speed fan which provides a variable volume air discharge by varying the speed of the fan, and wherein it is necessary to generate a rate of flow signal which is proportional to the amount of air delivered by the air circulating system in use, the improved method of generating said rate of flow signal comprising the steps of;

(i) generating a first signal which is proportional to the speed of the fan,

(ii) inputting the first signal to an input of a curve fitter which is programmed with the combined fluid delivery device/system speed/flow characteristic curves of the system and being adapted to receive said first signal and to generate a second signal which is proportional to fluid flow delivered by the fluid delivery device, said second signal being discharged at an output of said curve fitter.

According to one aspect of the present invention there is provided in a fluid circulating system which includes a conduit for conveying the fluid from a fluid delivery device which provides a variable volume fluid discharge by varying the speed of operation of the fluid delivery device and wherein it is necessary to generate a signal which is proportional to the volume of fluid delivered by a variable fluid volume fluid delivery device, the improved method of generating said control signal comprising the steps of;

(i) generating a first signal which is proportional to the speed of the fluid delivery device,

(ii) passing the first signal to a first input of a dual input curve fitter which is programmed with the combined fluid delivery device/system speed/flow characteristic curves of the system,

(iii) generating a second signal which is proportional to the pressure in the conduit, and

(iv) passing the second signal as a second input to the dual input curve fitter to offset the first signal prior to curve fitting and thereafter fitting the offset signal to the curve of the curve fitter to generate an output signal which is proportional to fluid flow delivered by the fluid delivery device.

According to a further aspect of the present invention there is provided in a fluid circulating system which includes a conduit for conveying the fluid from a fluid delivery device which provides a variable volume fluid discharge by varying the speed of operation of the fluid delivery device and wherein it is necessary to generate a signal which is proportional to the volume of fluid delivered by the fluid delivery device, the improvement of means for generating a fluid flow signal comprising;

(i) first signal generating means for generating a first signal which is proportional to the speed of the fluid delivery device,

(ii) second signal generating means adapted to generate a second signal which is proportional to the pressure in the conduit, and

(iii) dual input curve fitter having first and second inputs, said first input of said dual input curve fitter means communicating with said first signal generating means to receive said first signal, said second input of said dual input curve fitter means communicating with said second signal generating means to receive said second signal, said curve fitter means being programmed with the speed-fluid volume output curves of the selected variable fluid volume fluid delivery device, and being adapted to generate a third signal which is proportional to fluid flow delivered by the fluid delivery device.

According to one aspect of the present invention there is provided in an air conditioning system having a variable speed supply fan for supplying a variable volume of air through a supply duct by varying the speed of operation of the air fan, a method of generating a signal which is indicative of the volume of air supplied to the system through an air supply duct comprising the steps of:

(i) generating a first signal which is proportional to the speed of the air supply fan,

(ii) passing the first signal to a dual input curve fitter which is programmed with the speed-air volume output curves of the selected variable air volume air delivery device,

(iii) generating a second signal which is proportional to the pressure in the duct system, and

(iv) passing the second signal as a second input to the dual input curve fitter to generate a third signal which is proportional to air flow delivered by the air delivery device.

According to a further aspect of the present invention there is provided in a air conditioning system which includes a duct for conveying the air from a variable speed supply fan which provides a variable volume air discharge by varying its speed of operation and wherein it is necessary to generate a signal which is proportional to the volume of air delivered by the variable speed supply fan, the improvement of means for generating a control signal comprising;

(i) first signal generating means for generating a first signal which is proportional to the speed of the supply fan,

(ii) second signal generating means adapted to generate a second signal which is proportional to the pressure in the duct system, and

(iii) dual input curve fitter having first and second inputs, said first input of said dual input curve fitter means communicating with said first signal generating means to receive said first signal, said second input of said dual input curve fitter means communicating with said second signal generating means to receive said second signal, said curve fitter means being programmed with the speed-air volume output curves of the selected variable air volume air delivery device, and being adapted to generate a third signal which is proportional to air flow delivered by the air delivery device.

PREFERRED EMBODIMENT

The invention will be more clearly understood with reference to the following detailed specification read in conjunction with the drawings wherein:

FIG. 1 is a diagrammatic representation of a building having an air conditioning system of the type to which the present invention relates.

FIG. 2 is a block diagram illustrating a control system suitable for use in association with variable speed fans of an air conditioning system of the type illustrated in FIG. 1.

FIG. 3 is a diagram illustrating a variable air volume controller suitable for use in controlling the capacity of the supply fan and controlling the operation of the return fan of an air conditioning system.

FIG. 4 is a diagram illustrating a curve fitter suitable for use in the controller of FIG. 3.

FIG. 5 is a diagram illustrating a response curve of a typical controller system.

FIG. 6 is a diagram of a system for generating an offset signal to the controller when air exhaust systems are provided in the air space which is to be conditioned.

FIG. 7 is a graph showing percentage fan capacity versus fan speed of a typical supply fan.

FIG. 8 is a diagram illustrating a typical system curve of an air conditioning instalation, and

FIG. 9 is a diagram illustrating a typical fan curve of a variable speed fan upon which the plot of the system curve of FIG. 8 is superimposed.

The System Curve Equation (Pressure/Flow) which is characteristic of the duct system and which relates the total pressure in a system such as a fan system to the rate of flow of air in the system is well known.

Similarly fan curves (Pressure/Flow/Speed) which relate the speed of the fan to the pressure drop and to the flow rate of the fan have been available to fan users for many years. The fan curves and computer print-outs which provide similar information are provided by fan manufacturers.

I combine the information which is available in the System Curves, which are characteristic of the system, and the information which is available in the air circulating device curves, which are characteristic of the air circulating device, to determine Combined Air Circulating Device/System Characteristics of a Air Circulating System.

I can, for example, combine the information which is available in the System Curve of an air circulating system, which is characteristic of the system, and the information which is available in the Fan Curves, which are characteristic of the fan, to determine Combined Fan/System Characteristics of an air conditioning system or the like.

I can also combine the information which is available in the System Curve of liquid pumping system, which is characteristic of the system, and the information which is available in the Pump Curves, which are characteristic of the pump, to determine Combined Pump/System Characteristics of a liquid pumping system.

As previously indicated it is well known that the conditions under which air flow takes place in an air conditioning duct is subject to the following equation:

    dP=C.sub.1 q.sup.2 +C.sub.2 q.sup.1 +C.sub.3 q.sup.0       EQUATION 1

Where

C₁, C₂, C₃ are constants

q=air flow in suitable units

dP=pressure drop of duct system in suitable units.

EQUATION 1 breaks up the pressure drop into components due to totally turbulent flow depicted by the q² term; due to laminar flow depicted by the q¹ term; and a component independent of flow depicted by the q⁰ term. (Note q⁰ =1). Experience indicates that in the range of operation of most air conditioning systems of less than 50% capacity reduction (turndown) and low settings of the discharge pressure controller, the laminar flow component is usually negligible. If we assume this term to be zero, then EQUATION 1 simplifies to the following:

    dP=C.sub.1 q.sup.2 +C.sub.3 q.sup.0                        EQUATION 2

In air conditioning systems where the laminar flow component is not negligable, it must, of course, be taken into account by solving EQUATION 1.

On the other hand in a system where the pressure is not controlled and laminar flow does not exist in the normal operating range of the fan (i.e. C₂ =0); then Equation 1 may be further simplified as follows;

    dP=C.sub.1 q.sup.2 +C.sub.2 q.sup.1 +C.sub.3 q.sup.0       EQUATION 1

    dP=C.sub.1 q.sup.2 +0 +0

    dP=C.sub.1 q.sup.2                                         EQUATION 3

CURVE FITTER

A suitable curve fitter is illustrated in FIG. 4 of the drawings.

As previously indicated the fan speed and air flow in an air conditioning system may be expressed by the Equation 1 as follows:

    dP=C.sub.1 q.sup.2 +C.sub.2 q.sup.1 +C.sub.3 q.sup.0

Therefore;

    0=C.sub.1 q.sup.2 +C.sub.2 q.sup.1 +C.sub.3 q.sup.0 -dP    (EQUATION 4)

The theoretical relationship between the speed of a fan and the pressure rise across a fan and the relationship between the speed of a fan and the air flow of a fan is well known;

    i.e. S.sub.1 /S.sub.2 =q.sub.1 /q.sub.2

    and S.sub.1.sbsb.2.sup.2 /S.sub.2 =P.sub.1 /p.sub.2

Where S is the speed of the fan in RPM. Therefore; ##EQU1## and then the speed is at a maximum then ##EQU2## where K is a constant Therefore; dP=KS² in EQUATION 4

    0=C.sub.1 q.sup.2 +C.sub.2 q1.sup.1 +C.sub.3 q.sup.0 -KS.sup.2 EQUATION 5

The curve fitter 53 (FIG. 3) is designed to be programmed to solve EQUATION 5. With reference to FIG. 4 of the drawings it will be seen that the curve fitter 53 comprises a potentiometer 1 and a squaring amplifier 2 which are connected to a multiplier 3 which is in turn connected to a summer 4. A second potentiometer 5 and the line 15 (Q) are connected to a multiplier 6 which is in turn connected to summer 4. Static pressure line 17 is also connected to the summer 4. A squaring amplifier 7 and a potentiometer 8 are connected to a multiplier 9. The outputs of the summer 4 and multiplier 9 are connected to the inputs of a difference amplifier 11 which is in turn connected to integrator 13.

In use this curve fitter is programmed by dialing in the value of the constants C₁, C₂ and K to the potentiometers 1, 5 and 8 respectively. The multiplier 3 receives signals C₁ and Q₂ and multiplies the values to provide an output signal C₁ Q². The multiplier 6 receives signals Q and C₂ and generates an output signal C₂ Q to the summer 4. The signal C₃ is fed directly to an input of the summer 4. The summer 4 sums these signals to provide an output signal (C₁ Q² +C₂ Q+C₃) which is fed to the difference amplifier 11. Similarly the signal KS², which is the output from the multiplier 9, is fed to the other input of the difference amplifier 11.

If the two input signals to the difference amplifier 11 are equal, then the output signal from the difference amplifier 11 is zero, then the output of the integrator 13 is constant and this signal can be interpreted as a measure of the rate of flow of air through the air conditioning system. If the two input signals to the difference amplifier 11 are not equal then the output signal from the difference amplifier 11 is non zero. This error signal is integrated by integrator 13 to provide a feedback which will adjust the inputs to the summer 4 until the balance is restored in the difference amplifier 11, which has the effect of adjusting Q to equal the actual rate of flow signal. Thus when the signal Q, which is based on the speed of the fan, is stable, it is proportional to the actual rate of flow of air.

EXAMPLE 1

In a typical air conditioning application, where the pressure is not controlled and laminar flow does not exist the ducting system is designed by an engineering contractor. The engineering contractor also specifies the fan to be used in association with the system. Typically, the designer of a control system may be advised that the fan which is to be used is designed to deliver 61,200 cfm at 5" w.g.

With this information, I can proceed to design a control system which will have a substantially greater accuracy and stability when utilizing a variable speed fan to control the rate of flow of air.

In this example, where the value of "q" (rate of flow) is high and where the pressure is not controlled and laminar flow does not exist, EQUATION 3 may be used to establish the System Curve.

At maximum air flow the system is designed to convey 61,200 CFM of air when overcoming a duct pressure of 5" WG. therefore:

in EQUATION 3, when dP=5", we have;

    5=C.sub.1 (61,200).sup.2,

therefore:

C₁ =5/(61,200)²

Therefore Equation 3 provides: ##EQU3##

Thus, air flow in this type of duct system is in accordance with the Equation 3, which can now be solved for flow rates within the stable operating conditions of the system such as 100% to 40% in 10% increments.

For example when 90% flow rate required; ##EQU4##

With this information the System Curve A of FIG. 8, (Pressure/Flow) may be plotted or a System Table (Pressure/Flow) may be tabulated.

The following TABLE 1 is a typical System Table which can be prepared by repeating the foregoing at 10% increments in reduction of air flow capacity.

                  TABLE 1                                                          ______________________________________                                         AIR FLOW (C.F.M.)                                                              ACTUAL      %       PRESSURE (ins.W.G.)                                        ______________________________________                                         61,200       100    5                                                          55,080      90      4.05                                                       48,960      80      3.2                                                        42,840      70      2.45                                                       36,720      60      1.8                                                        30,600      50      1.25                                                       24,480      40      0.8                                                        ______________________________________                                    

I am now in a position to plot the System Curve A (FIG. 8) on the Fan Curves (FIG. 9) of the selected fan and the point at which the System Curve intersects the speed curves (FIG. 9) is noted and tabulated to provide Table 2 as follows;

                  TABLE 2                                                          ______________________________________                                         AIR FLOW (C.F.M.)                                                                              PRESSURE   FAN SPEED                                           ACTUAL    %         (ins.W.G.) (rpm)                                           ______________________________________                                         61,200     100      5          587                                             55,080    90        4.05       523                                             48,960    80        3.2        462                                             42,840    70        2.45       409                                             36,720    60        1.8        351                                             30,600    50        1.25       289                                             24,480    40        0.8        231                                             ______________________________________                                    

With this information, I can now obtain a Curve C (FIG. 7) of air flow/fan speed for the condition where the pressure in the duct is not controlled. Thus, I can establish the speed at which the fan should run in order to provide any required percentage of flow capacity when the pressure in the duct system is not controlled.

In practice the fan curves which are provided by the fan manufacturer may not accurately reflect the conditions which prevail in a particular instalation. In these circumstances it is necessary to take readings of the actual air flow in the duct of the system in order to determine Points P1 and P2' to obtain a modified Curve C' (FIG. 7). This is information which is commonly provided by the System Balancing Contracter. These measurements provide the fan speed and air flow at maximum and minimum conditions which can be used to plot Points P1 and P2' of Curve C' of FIG. 7. Thus Curve C' of FIG. 7 is a typical "Actual System Fluid Flow Curve" and Curve C is a "Theoretical System Fluid Flow Curve". The Curve C' and the Curve C may be substantially identical in well designed fluid circulating systems.

I know that the limiting case of the path P1-P2' is a straight line, and further that a further Point 3 cannot be above this straight line (P1-P2'), although it may be below the straight line (P1-P2'). If the third point (Point 3) can be obtained from the Balancing Contracter it would greatly increase the accuracy of path P1-P2'.

The theoretical relationship between the speed of a fan and the pressure rise across a fan and the relationship between the speed of a fan and the air flow of a fan is well known; ##EQU5##

Thus, as a first approximation I can determine the relationship between the air flow output of a fan and its speed (Curve C' FIG. 7) which is the "System Fluid Flow Curve" from which the "System Fluid Flow Data" may be obtained. This relationship does permit me to utilize the speed of the fan to generate a signal which is proportional to air flow. In my control system I provide a curve fitter, which may be in the form of an amplifier or a digital computer or the like which I program with the System Fluid Flow Curves or System Fluid Flow Data which I have previously developed as described above. I am then able to input a signal to the curve fitter which is proportional to the speed of the fan which is processed by the curve fitter to generate an output signal which is proportional to the actual rate of flow in the system.

My system may also be employed in an air or liquid circulating system of a building which has a building automation computer to monitor and control the operations of these systems. This type of computer may be programmed to accept the speed input signal from a fan or pump and to calculate air flow (C.F.M.) or liquid flow (G.P.M.).

The foregoing Example relates to a system in which the pressure in the system is not controlled.

If a fan is attached to an air conditioning system consisting of filters, coils, ducts, terminal boxes, dampers, etc., air flow will take place at the point where the System Curve intercepts the Fan Curve. If the system is a constant volume system, there would be one fan curve depicting the head-flow condition at a particular constant speed. In a Variable volume instalation there are many system curves between the curve depicting minimum flow and the curve depicting maximum flow.

Each time a damper changes position, resulting in a different pressure in the duct, flow would be affected. Since air flow can only take place at the point of intersection of the fan curve and the system curve, if the duct resistance changes the System Curve will change. Hence, there can be many System Curves within the definable limits of maximum and minimum flow.

If the fan is to vary capacity, there would likewise be an infinite number of fan characteristic curves between minimum and maximum capacity; one for each speed. The fan system operation is somewhere in the region defined by the minimum capacity-flow and the maximum capacity-flow condition which is determined by the system demand. That is to say the minimum capacity flow is that which results when the load demand is at a minimum and the maximum capacity-flow results when the load demand is at design conditions.

If the system curve follows EQUATION 1 or the simplified EQUATION 2, then an accurate graph of fan speed versus air flow may be obtained. In variable speed systems, a signal proportional to speed is easily obtained. Since this graph is linear for at least part of its range, it can be used to read out air flow directly within the linear range. The zero flow offset is the value of the measured pressure in the duct. This is easily obtained from the static pressure controller specifically from the pressure sensor output after signal conditioning or from the set point circuit. Therefore, an inexpensive and accurate method of indicating air flow can be obtained.

EXAMPLE 2

In a typical air conditioning application, the ducting system is designed by an engineering contractor. The engineering contractor also specifies the fan to be used in association with the system. The System Balancing Engineer will provide the data which includes the actual pressure and speed of flow at the specified maximum and minimum flow rates. Typically, the designer of a control system may be advised that the fan which is to be used is designed to deliver 61,200 cfm at 5" w.g. and the pressure in the duct system is to be controlled to 11/4 " w.g. When such a system has been balanced the Balancing Engineer may typically report that, at the actual minimum flow the fan must deliver 25,000 c.f.m. of air at 2.1" w.g. while rotating at 335 r.p.m.

With this information, I can proceed to design a control system which will have a substantially greater accuracy and stability when utilizing a variable speed fan to control the rate of flow of air.

In this example, where the value of "q" (rate of flow) is high, EQUATION 2 may be used to establish the System Curve.

At the condition where no air flows through the duct, the pressure at the inlet to the duct will equal the control pressure, namely 11/4" w.g.;

therefore:

in EQUATION 2, when dP=11/4" and q=0, we have;

    11/4"=C.sub.1 (0)+C.sub.3,

therefore: C₃ =11/4 (i.e. the setting of the pressure controller)

If we now assume the air flow to be 61,200 cfm, at a pressure (dP) of 5" w.g., we find that Equation 2 provides: ##EQU6##

Thus, air flow in the typical duct system is in accordance with the Equation 2, which can now be solved for flow rates within the the stable operating conditions of the system such as 100% to 40% in 10% increments.

Using this equation, we can therefore develop System Curve B (FIG. 8) which provides an indication of pressure (dP)/air flow rate (q).

As discussed above, the 100% air flow capacity is predetermined, namely 61,200 cfm at 5" w.g.

Using Equation 2, we can now determine the required pressure drop for various reductions in air flow as for example, 90% to 40% in 10% increments.

At 90% air flow capacity, q=(0.9×61,200) cfm, therefore: ##EQU7##

The following TABLE 3 can be established by repeating the foregoing at 10% increments in reduction of air flow capacity.

                  TABLE 3                                     effecting automatic release of the antenna assembly from the      projectile upon impact thereof.

Yet another object of the present invention is to provide an improved release assembly for an antenna assembly of a terminal delivery vehicle of reliable repetitive deployment capability.

SUMMARY OF THE INVENTION

These and other objects of the present invention are achieved by a release assembly mounted within a housing member for maintaining an antenna assembly under spring deployment compression in a terminal delivery vehicle for delivery by a projectile and wherein the release assembly is comprised of a cover member and a weight member under compressive spring forces to maintain a locking ring spring within a groove of the housing member and wherein upon impact of the TDV the inertia of the weight member against the cover member causes the locking ring spring to be withdrawn from within the groove in the housing member, thereby to free the release member from the housing member and permitting activation of the deployment compressive spring forces for deploying the antenna assembly from the terminal delivery vehicle.

BRIEF DESCRIPTION OF THE DRAWINGS

Further objects and advantages of the present invention will become apparent from the following detailed description of an embodiment thereof especially, when taken with the accompanying drawings, wherein:

FIG. 1 is a cross-sectional view of a housing member for a projectile illustrating the present invention;

FIG. 2 is a cross-sectional view of the release assembly in compressed configuration;

FIG. 3 is a front view of the release assembly; and

FIG. 4 is an elevational view of the TDV with antenna deployment.

DETAILED DESCRIPTION OF THE DRAWINGS

Referring now to the drawings, and particularly to FIG. 1, there is illustrated a housing member for a terminal delivery vehicle assembly for positioning within a projectile assembly (not shown), generally indicated as 10, and including a base member, generally indicated as 12, in which is positioned a spring loaded antenna assembly, generally indicated as 14, maintained within the housing assembly 10 by an antenna release assembly, generally indicated as 16, resiliently mounted within the base member 12, as more fully hereinafter discussed.

The base member 12 is formed of a generally cylindrically-shaped body portion 20 and an end flange portion 22 including an end surface 24. The body portion 20 of the base member 12 is formed with a plurality of cylindrically-shaped interior surfaces 26, 28, 30, and 32 (from left to right) of varying diameters defining a chamber 34, referring particularly to FIG. 1.

Interior surface 26 is of a great diameter than interior surface 28 which is of a smaller diameter than interior surface 30 thereby defining an intermediate flange member 36 including a shoulder portion 38 for a portion of the chamber 34 defined by the interior surface 28. The interior surface 32 is slightly larger than the interior surface 30 thereby defining a shoulder portion 40 proximate the end flange portion 22.

The interior surface 32 of the housing member 10 is formed with a groove 42 extending circumferentially therearound. From the interior surface 32, there is formed a frusto conically-shaped surface 44 extending outwardly toward the end surface 24 of the end flange portion 22 of the base member 12.

The antenna release assembly 16 is comprised of a cover member 50 including a disc-shaped end portion 52 and a shaft portion 54 extending perpendicularly therefrom and formed with a centrally-disposed channel 56 extending therethrough. About an outer surface 58 of the shaft portion 54, there is formed a circumferentially-extending groove 60. The cover member 50 is formed with a plurality of outwardly-extending sector portions 62 about a periphery of the disc-shaped end portion 52 defining therebetween opened sector areas 64. The sector portions 62 are formed with a groove 66 disposed about a peripheral surface thereof and in a plane perpendicular to the axis of the cover member 50.

The antenna release assembly 16 is further comprised of a weight member 70 including a disc-shaped portion 72 including a bore 74 defining a shoulder portion 76 with a bore 78 of a diameter slightly larger than the bore 74 thereof. About a periphery of the disc-shaped portions 72 the weight member 70 is formed with a plurality of sector-shaped arm members 80 extending in a direction parallel to the axis of the weight member 70. About a peripheral surface of each of the arm members 80, there is formed a channel 82 defined by arc-shaped parallelly-disposed outer and inner ridge elements 84 and 86. The arm members 80 of the weight member 70 are dimensioned to cooperate with the sector areas 64 of the cover member 50 as more fully hereinafter discussed.

The weight member 70 is positioned on the shaft portion 54 of the cover member 50 after positioning of a spring assembly 88 into a compressed mode about the shaft portion 54 by the interrelationship of said members and is maintained thereon by positioning a retaining ring 90 in the groove 60 formed in the outer surface 58 of the shaft portion 54 of the cover member 50. In such configuration, the cover member 50 and weight member 70 are maintained apart from each other limited by the retaining ring 90 and may be compressed together into an armed position against the compression spring forces of the spring assembly 88. In the armed position, as illustrated in FIG. 1, the outer ridge element 84 of the arm members 80 of the weight member 70 are coincident with the peripheral groove 66 formed in each of the sector portions 62 and form a groove of a larger diameter than the groove 66 as more fully hereinafter discussed.

The antenna assembly 14 is comprised of upper and lower band members 92 and 94 mounted together by intermediate member 96, and as illustrated in FIG. 4, are in an uncoiled mode. In FIG. 1, the upper and lower band members 92 and 94 are in a coiled mode ready for deployment.

The housing member 10 is mounted to a base of a terminal delivery vehicle (not shown), referring now to FIG. 1, after the assembly of the component parts of the housing member 10. The antenna assembly 14 is positioned within a sleeve member 102 including locking screws 104 and is disposed within the chamber 34 of the base member 12 and a holding plate 106 disposed thereon. Thereafter the antenna release assembly 16 is positioned within the channel 34 with the cover member 50 in contact with the holding plate 106, such that a split locking ring 108 under compression is positioned in the groove 42 and about an outer surface of inner ridge element 86 of the weight member 70, with the cover member 50 and weight member 70 in an opened position. Further assembly of the complete projectile assembly will be understood by one skilled in the art, as well as the launch of the projectile of such projectile assembly, including the terminal delivery vehicle.

The terminal delivery vehicle is separated from the launching projectile at a predetermined time after the launch as determined by ballistic trajectory, etc., to cause the terminal delivery vehicle with the aid of terra brakes 110 to impact into a predetermined area and stop thereby in the surface thereof. Upon impact, the inertia of the weight member 70 against the compressive forces of spring assembly 88 causes the weight member 70 to move towards the cover member 50 whereby the split locking spring 108 in the groove 42 under compressive forces in an outwardly and radially expanded direction and disposed about the outer surface of the inner ridge element 86 is permitted to assume a circular configuration in the groove 42 of the weight member 70 and thereby withdraw from the groove 42 in the base member 12 thereby to permit separation of the antenna release assembly 16 from the base member 12. Separation of the antenna release assembly 16 from the base member 12 permits deployment of the antenna assembly 14, in particular the upper and lower band members 92 and 94, referring now to FIG. 4, as a result of the band members being under coiled spring tension in the assembled configuration as illustrated in FIG. 1.

While the invention herein has been described in conection with an exemplary embodiment thereof, it will be understood that many modifications will be apparent to those of ordinary skill in the art and that this application is intended to cover any adaptations or variations thereof. 

What is claimed:
 1. In a terminal delivery vehicle having a base member including a storage chamber for an antenna assembly disposed in coiled configuration wherein said base member includes an end chamber of larger diameter than said storage chamber, a stowage and release assembly for retaining said antenna assembly in said storage chamber until deployment which comprises:a cover member; a weight member positioned for axial movement with respect to said cover member; means for limiting movement of said weight member with respect to said cover member; means for maintaining said members in spaced apart relationship; and means for mounting said storage and release assembly within said end chamber of said base member of said terminal delivery vehicle.
 2. The stowing and release assembly as defined in claim 1 wherein said cover member includes a shaft portion formed with a groove and wherein said weight member is formed with a base for positioning on said shaft of said cover member and wherein said means for limiting movement is a retaining ring disposed in said groove of said cover member.
 3. The stowing and release assembly as defined in claim 2 wherein said end chamber of said base member is formed with an inwardly-extending groove for receiving a retaining ring under compression upon positioning said stowage and release assembly in said end chamber.
 4. The stowing and release assembly as defined in claim 3 wherein said weight member is provided with arm portions for cooperating with and for maintaining said retaining ring under compression.
 5. The stowing and release assembly as defined in claim 4 wherein said means for maintaining said members in spaced apart relationship is a coil spring.
 6. The stowing and release assembly as defined in claim 4 wherein said arm portion of said weight member is provided with a peripherally-formed groove and wherein said cover member is provided with arm portions having a peripherally-formed groove whereupon compression of said weight member with respect to said cover member permits said retaining ring to snap into said grooves and thereby free said stowage and release assembly from said base member.
 7. The stowing and release assembly as defined in claim 6 wherein said cover member and said weight member are provided with open sector portions for cooperating with arm portions of respective members. 